首页|基于体积力模型的跨声压气机进气畸变数值模拟

基于体积力模型的跨声压气机进气畸变数值模拟

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为快速评估进气畸变对压气机气动性能的影响,发展了一种基于体积力模型的进气畸变三维数值模拟方法.首先研究了体积力源项的建模理论和方法,并将该模型嵌入商业软件CFX中对Darmstadt单级跨声压气机在均匀进气条件下进行了计算及验证.进一步利用该方法对压气机在180°总温、总压畸变条件下的特性及流场进行了数值模拟,结果表明:该方法能再现进气畸变对压气机特性的影响,同时压气机内部畸变流场强三维特征与URANS(全环非定常)结果基本保持一致;在总温和总压畸变条件下,压气机与上游畸变流场的耦合作用趋势相反.相比URANS计算,该方法对计算资源的消耗能降低5个数量级,并能有效捕捉畸变流场在压气机内部的传递特征.
Numerical simulation of transonic compressor with inlet distortion based on body-force model
In order to numerically study the impact of distorted inflow on a transonic compressor with less computational costs,a three-dimensional simulation method was developed based on body-force model(BFM).Firstly,the modeling method of building body-force source term was studied.The test data of the Darmstadt transonic compressor were used to verify the body-force model in performance prediction of the blade rows with clean inflow.Furthermore,steady simulations with a 180° circumferential total temperature and total pressure distortion were performed using BFM.This showed that the BFM can reproduce the distorted compressor characteristics.The evolution of the inlet distortion through the compressor and the circumferential phase change of the total temperature across the rotor were in line with unsteady Reynolds averaged Navier-Stockes(URANS).Under inlet total temperature and pressure distortion,the coupling trend of compressor and upstream distorted flow field was opposite.Compared with URANS,the BFM can significantly reduce the computational costs by 5 orders of magnitude while effectively capturing the main flow features inside the compressor.

compressorinlet distortionrapid assessmentbody-force modelcoupling effectaerodynamic performance

邱佳慧、杨晨、赵红亮、张敏、杜娟、聂超群

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中国科学院工程热物理研究所先进燃气轮机实验室,北京 100190

中国科学院先进能源动力重点实验室,北京 100190

中国科学院轻型动力创新研究院,北京 100190

中国科学院大学工程科学学院,北京 100049

华北电力大学能源动力与机械工程学院,北京 102206

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压气机 进气畸变 快速评估 体积力模型 耦合作用 气动性能

国家自然科学基金国家自然科学基金国家重大科技专项

51922098517905102017-Ⅱ-0004-0017

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(8)